Invention Grant
- Patent Title: Aircraft engine assembly with a supply path to an inter-flow compartment tank of turbine engine
-
Application No.: US17044412Application Date: 2019-04-02
-
Publication No.: US11572833B2Publication Date: 2023-02-07
- Inventor: Antoine Elie Hellegouarch , Frédéric Paul Eichstadt , Quentin Matthias Emmanuel Garnaud
- Applicant: SAFRAN AIRCRAFT ENGINES
- Applicant Address: FR Paris
- Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee: SAFRAN AIRCRAFT ENGINES
- Current Assignee Address: FR Paris
- Agency: Pearne & Gordon LLP
- Priority: FR1852926 20180404
- International Application: PCT/FR2019/050757 WO 20190402
- International Announcement: WO2019/193274 WO 20191010
- Main IPC: F02C7/06
- IPC: F02C7/06 ; B64D27/12 ; F01M11/04 ; F02C7/20 ; F02C7/32 ; F01D25/18 ; B64D27/26
Abstract:
An aircraft engine assembly includes a dual-flow turbine engine, a pylon for mounting the turbine engine, thrust-absorbing rods connecting the turbine engine to the pylon, and an inter-flow compartment housing a lubricant tank. In order to facilitate the filling of the tank, a lubricant supply path is fluidly connected to the tank, this path passing through an inner hollow region of at least one of the two thrust-absorbing rods.
Public/Granted literature
- US20210115852A1 AIRCRAFT ENGINE ASSEMBLY WITH A SUPPLY PATH TO AN INTER-FLOW COMPARTMENT TANK OF TURBINE ENGINE Public/Granted day:2021-04-22
Information query
IPC分类:
